CN109283548B - Laser angle measurement system and anti-backscattering method - Google Patents

Laser angle measurement system and anti-backscattering method Download PDF

Info

Publication number
CN109283548B
CN109283548B CN201810779168.5A CN201810779168A CN109283548B CN 109283548 B CN109283548 B CN 109283548B CN 201810779168 A CN201810779168 A CN 201810779168A CN 109283548 B CN109283548 B CN 109283548B
Authority
CN
China
Prior art keywords
signals
target
processor
measurement system
laser
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201810779168.5A
Other languages
Chinese (zh)
Other versions
CN109283548A (en
Inventor
孙宏宇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xi'an Raytheon Defense Technology Co ltd
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201810779168.5A priority Critical patent/CN109283548B/en
Publication of CN109283548A publication Critical patent/CN109283548A/en
Application granted granted Critical
Publication of CN109283548B publication Critical patent/CN109283548B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S17/00Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/88Lidar systems specially adapted for specific applications
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/26Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/481Constructional features, e.g. arrangements of optical elements
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/495Counter-measures or counter-counter-measures using electronic or electro-optical means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Electromagnetism (AREA)
  • Optical Radar Systems And Details Thereof (AREA)

Abstract

The laser angle measurement system for resisting back scattering includes a position marker and an electronic cabin, wherein the position marker consists of an optical device and a detector; the electronic cabin consists of a front-end circuit, a switch circuit, a high-speed acquisition circuit, a processor and a power supply; the processor is connected with the switch circuit; the anti-backscattering method comprises the steps of: 1) The laser pulse with the period of 50ms optically receives back scattering and target echo signals through atmospheric attenuation and target diffuse reflection; 2) The processor performs waveform matching to search for a target signal, and the gate is in an open state and is converted into a digital signal; 3) The processor performs waveform matching on the digital signals, and if successful, closes the wave gate and simultaneously opens the timer; if not, continuing to acquire signals to carry out waveform matching; 4) After successful matching, opening a wave gate until 49.999ms, calculating angle information, filtering back scattering and interference signals, and collecting only target echo signals; 5) Guan Bomen by 50ms, recounting, repetitions 4) and 5); high sensitivity and high anti-interference capability.

Description

Laser angle measurement system and anti-backscattering method
Technical Field
The invention belongs to the technical field of laser angle measurement systems, and particularly relates to a laser angle measurement system and a backscattering resistance method.
Background
The laser angle measurement system tracks the target by receiving the laser echo reflected by the target diffusely, and the information detection and processing methods adopted by most laser angle measurement systems or the received information quantity have limited target identification capability and are insufficient for judging whether the target is tracked. As long as it is within the detection field of view, which signal energy is large, precisely where the laser spot is, tracks which.
For the target detection of the signal received by the interference detection system due to the atmospheric scattering, the angle measurement system can easily identify that the atmospheric backscattering is the target, and especially when the atmospheric environment is very bad, the backscattering of the atmosphere is serious, and the signal of the atmospheric backscattering can be larger than the signal reflected by the target, so that the signal returned by the atmosphere is mistakenly regarded as the energy signal reflected by the target, and the laser angle measurement system can not track the target normally.
Therefore, in order to obtain higher capturing precision, the laser angle measurement system needs to filter out the atmospheric back scattering echo signal and the induced signal, and identify the real target echo pulse signal so as to meet the missile guidance requirement.
At present, only the Chinese aerospace aerodynamic technical institute utilizes a distance wave gate technology to inhibit interference caused by atmospheric backscattering to capturing a target signal by an angle measurement system, and backward scattered light and target reflected light at different distances are separated according to time sequence, but a synchronous signal sent by a missile fire control system is needed, so that the difficulty is increased in application.
Disclosure of Invention
In order to solve the problems, the technical scheme of the invention is as follows: a laser angle measurement system and a method for resisting backscattering, wherein the laser angle measurement system utilizes the laser diffusely reflected by a target to automatically intercept and track a ground fixed/moving target; meanwhile, a target sight angle signal (azimuth and pitching) relative to the missile axis is provided for the missile autopilot, so that the missile can be guided automatically until a target is hit.
In order to achieve the above purpose, the invention adopts the following technical scheme:
the laser angle measurement system for resisting back scattering includes a position marker and an electronic cabin, wherein the position marker consists of an optical device and a detector; the electronic cabin consists of a front-end circuit, a switch circuit, a high-speed acquisition circuit, a processor and a power supply;
the optical device is connected with the detector; the detector is connected with the high-speed acquisition circuit through the front-end circuit; the high-speed acquisition circuit is connected with the bullet loading machine through the processor;
the GPIO terminal of the processor is connected with the switch circuit.
The processor is connected with the bullet machine through a communication interface.
The power supply is electrically connected with the detector, the front-end circuit, the switching circuit, the high-speed acquisition circuit and the processor to supply power to all circuits of the angle measuring system.
The optical device is arranged at the front end of the angle measurement system and comprises a narrow-band optical filter and a plurality of optical mirrors, the narrow-band optical filter only allows the used laser wavelength to penetrate and remove clutter interference, and the plurality of optical mirrors are used for collecting and converging laser signals, wherein the laser signals comprise target reflected light and backward scattered light.
The front discharging circuit adopts ADA4817 chip and AD8336 chip of AD company to condition and amplify current signal, and the design of the front discharging circuit makes the system have large dynamic range and perform automatic gain control because the signal increases sharply with decreasing distance.
The switching circuit adopts a FAIRCHILD company FA66 chip, is connected with the front discharge circuit, is controlled by the processor to be only started when a laser signal arrives after target identification, and is closed at other times, so that backward scattering and clutter interference can be effectively filtered.
The high-speed acquisition circuit adopts an AD9239 chip of an AD company, is connected with the switch, and effectively samples the pulse electric signal after detecting the pulse of the pulse electric signal, so as to ensure the sample hold and output of the laser pulse electric signal when the wave gate is opened.
The optical signals processed by the optical device are converged on the detector, the detector converts the optical signals into current signals, the offset and the offset azimuth of the target relative to the optical axis are measured by using a four-quadrant element, when the target offsets the optical axis, the laser energy is distributed unevenly on the four quadrants, and the offset can be obtained through sum and difference operation. The linear range is adjusted by adjusting the size of the light spot, the defocus amount of the four-quadrant element, and the like.
The collected signals can identify the correct target signals through a software internal algorithm of a processor connected with a high-speed collection circuit. After identification, the time of the identified target signal is taken as a reference, the arrival time of the target signal is further predicted, so that the control wave gate is opened only when the target signal arrives, and the wave gate is closed at other times, thereby achieving the purpose of removing the backward scattering interference and solving the problem that the accurate guidance cannot be realized due to the fact that the control wave gate is opened only when the target signal arrives.
The anti-back scattering laser angle measurement system is connected with the on-board machine through the communication interface of the processor, and feeds back the measured angle and other information to the on-board machine through the communication interface.
A method for resisting backscatter using a laser goniometer system, comprising the steps of:
step 1, a laser emits laser pulses with the period of 50ms, and through atmospheric attenuation and target diffuse reflection, the optical reception of an angle measurement system is backward scattering and target echo signals;
step 2, the processor of the angle measurement system performs waveform matching on the high-speed collected signals to search for target signals, at the moment, the wave gate is in an open state, the optical signals received by the angle measurement system are converted into digital signals by the high-speed collection circuit after photoelectric processing of the detector, and the processor performs waveform matching on the obtained digital signals
a. If the matching is successful, closing the wave gate and simultaneously starting a timer;
a filter is defined by the impulse response h (t) and taken
h(t)=s(-t),-T≤t≤0
For a received signal r (T) to be processed at 0T T, the response of the matched filter is g (T):
this gives:
wherein S is a test statistic, that is, the output S of the correlation receiver is the result of sampling the output of the matched filter at the starting point t=0 of the observation area; u is the integral of t, t is the variable, u is the integral;
the actual target echo signal s (t) signal is a discrete digital sequence s (n) after high-speed acquisition, the received signal r (t) is a sequence r (n), and similarly, the response of the matched filter is g (n):
this gives:
b. if the matching is unsuccessful, continuing to acquire signals to carry out waveform matching;
step 3, after the matching is successful, a timer of the processor counts 49.999ms and then opens a wave gate, the processor processes the signals acquired at high speed to calculate angle information, and at the moment, the backscattering and interference signals are filtered, and only target echo signals are acquired;
step 4, the timer counts up to 50ms Guan Bomen, and the timer restarts counting, and then steps 3 and 4 are repeated continuously.
The beneficial effects of the invention are as follows:
the anti-back scattering laser angle measurement system automatically intercepts and tracks the ground fixed/moving target by utilizing the laser diffusely reflected by the target. Meanwhile, a target sight angle signal (azimuth and pitching) relative to the missile axis is provided for the missile autopilot, so that the missile can be guided automatically until a target is hit. According to the detection method of the laser angle measurement system, a synchronous signal is not needed, so that the laser angle measurement system overcomes and eliminates the atmospheric scattering interference to realize accurate guidance.
The laser angle measurement system for resisting back scattering consists of a position marker and an electronic cabin, wherein the position marker is used for collecting and converging laser and converting the laser into a current signal, and the electronic cabin is used for conditioning, amplifying and collecting the current signal. The acquired signals identify the correct target signals through an internal algorithm of software, so that the arrival time of the target signals is further predicted, the control wave gate is opened only when the target signals arrive, the aim of removing the backward scattering interference is achieved, and the problem that accurate guidance cannot be achieved due to the fact that the backward scattering interference is solved.
When backscattering exists, post-injection interception can be realized; the limitation on the use environment is reduced, and the same-machine irradiation without included angles can be realized; high sensitivity and strong anti-interference capability.
Brief description of the drawings
Fig. 1 is a schematic block diagram of the circuit of the present invention.
Fig. 2 is a flow chart of the present invention.
FIG. 3 is a schematic representation of the response of the anti-backscatter system of the present invention.
Fig. 4 is a diagram of an actual waveform obtained by sampling at a high speed in an embodiment of the present invention.
Detailed Description
The structural principles, procedures and working principles of the present invention are described in further detail below with reference to the drawings and examples.
The back scattering resisting laser angle measuring system has the circuit structure shown in figure 1 and includes one position marker comprising optical device and detector and electronic cabin; the electronic cabin consists of a front-end circuit, a switch circuit, a high-speed acquisition circuit, a processor and a power supply;
the optical device is connected with the detector; the detector is connected with the high-speed acquisition circuit through the front-end circuit; the high-speed acquisition circuit is connected with the bullet loading machine through the processor;
the GPIO terminal of the processor is connected with the switch circuit.
The processor is connected with the bullet machine through a communication interface.
The power supply is electrically connected with the detector, the front-end circuit, the switching circuit, the high-speed acquisition circuit and the processor to supply power to all circuits of the angle measuring system.
The optical device is arranged at the front end of the angle measurement system and comprises a narrow-band optical filter and a plurality of optical mirrors, the narrow-band optical filter only allows the used laser wavelength to penetrate and remove clutter interference, and the plurality of optical mirrors are used for collecting and converging laser signals, wherein the laser signals comprise target reflected light and backward scattered light.
The current signal is conditioned and amplified by the front amplifying circuit, and the design of the front amplifying circuit ensures that the system has a large dynamic range and performs automatic gain control because the signal is increased sharply along with the decrease of the distance.
And after the pulse electric signal pulse is detected by the high-speed acquisition circuit connected with the switch, the pulse electric signal is effectively sampled, so that the sampling, holding and outputting of the laser pulse electric signal when the wave gate is opened are ensured.
The switch circuit connected with the front discharge circuit is controlled by the processor to be turned on only when a laser signal arrives after the target is identified, and turned off at other times, so that backscattering and clutter interference can be effectively filtered.
The optical signals processed by the optical device are converged on the detector, the detector converts the laser signals into current signals, the four-quadrant elements are used for measuring the offset and the offset azimuth of the target relative to the optical axis, when the target offsets the optical axis, the laser energy is distributed unevenly on the four quadrants, and the offset can be obtained through sum and difference operation. The linear range is adjusted by adjusting the size of the light spot, the defocus amount of the four-quadrant element, and the like.
The collected signals can identify the correct target signals through a software internal algorithm of a processor connected with a high-speed collection circuit. After identification, the time of the identified target signal is taken as a reference, the arrival time of the target signal is further predicted, so that the control wave gate is opened only when the target signal arrives, and the wave gate is closed at other times, thereby achieving the purpose of removing the backward scattering interference and solving the problem that the accurate guidance cannot be realized due to the fact that the control wave gate is opened only when the target signal arrives.
The anti-back scattering laser angle measurement system is connected with the bullet upper machine through the communication interface of the processor, and feeds back the measured angle and other information to the bullet upper machine through the communication interface.
The back scattering resisting method with laser angle measuring system includes the following steps:
step 1, a laser emits laser pulses with the period of 50ms, and through atmospheric attenuation and target diffuse reflection, the optical reception of an angle measurement system is backward scattering and target echo signals;
step 2, a processor of the angle measurement system performs waveform matching on the signals acquired at high speed to search for target signals, at the moment, the wave gate is in an open state, optical signals received by the angle measurement system are converted into digital signals by a high-speed acquisition circuit after photoelectric processing of the detector, and the processor performs waveform matching on the obtained digital signals:
a. if the matching is successful, closing the wave gate and simultaneously starting a timer;
a filter is defined by the impulse response h (t) and taken
h(t)=s(-t),-T≤t≤0
For a received signal r (T) to be processed at 0.ltoreq.t.ltoreq.T, the response of the matched filter is:
this gives:
wherein S is a test statistic, that is, the output S of the correlation receiver is the result of sampling the output of the matched filter at the starting point t=0 of the observation area; u is the integral of t, t is the variable, u is the integral;
the actual target echo signal s (t) is a discrete digital sequence s (n) after high-speed acquisition, the received signal r (t) is a sequence r (n), and similarly, the response of the matched filter is as follows:
this gives:
b. if the matching is unsuccessful, continuing to acquire signals to carry out waveform matching;
step 3, after the matching is successful, a timer of the processor counts 49.999ms and then opens a wave gate, the processor processes the acquired signals acquired at high speed to calculate angle information, and at the moment, the backward scattering and interference signals are filtered, and only the target echo signals are acquired;
step 4, the timer counts up to 50ms Guan Bomen, and the timer restarts counting, and then steps 3 and 4 are repeated continuously.
The angle measurement system starts searching work, can detect back scattering and target echo, matches according to the waveform characteristics of the echo signals, and judges whether the echo signals are echo signals or not.
The laser pulse signal emitted by the laser is delta (t), and after the atmospheric attenuation, the diffuse reflection of the target and the photoelectric treatment of the angle measurement system, the target echo is s (t), as shown in the response schematic diagram of the system in fig. 3. The system output target echo s (t) under the action of the laser pulse signal delta (t) is the convolution of the input of the system and the response h (t) of the system, namely delta (t) ×h (t) =s (t), and since the convolution of any signal and the impact function is itself, h (t) =s (t).
A filter is now defined by the impulse response h (t) and taken
h(t)=s(-t),-T≤t≤0
For a received signal r (T) to be processed at 0.ltoreq.t.ltoreq.T, the response of the matched filter is:
this gives:
wherein S is a test statistic, that is, the output S of the correlation receiver is the result of sampling the output of the matched filter at the starting point t=0 of the observation area;
the actual target echo signal s (t) is a discrete digital sequence s (n) after high-speed acquisition, the received signal r (t) is a sequence r (n), and similarly, the response of the matched filter is as follows:
this gives:
the sampling rate of the high-speed sampling circuit is 500MHz, the pulse width of an s (t) signal is 600ns, and the number of points N=300 of the obtained sequence s (N); after the sequence normalization processing of the actual sampling, setting S through matched filtering calculation t =30, the probability of interception is greater than 98%.
If an echo signal can be identified (S > S) t 30), starting time counting, wherein the starting value is the moment when the laser pulse reaches the angle measurement system, and the counting mode is incremental counting; if the echo signal cannot be identified (S < S t =30), the search is continued. The time counting value is 49.999ms, a wave gate is opened, and at the moment, the target echo reaches the angle measurement system, and the angle measurement system receives the target echo signal and outputs the target echo signal after signal processing, conditioning and amplifying and acquisition; and closing the wave gate immediately after the target echo arrives at the angle measurement system, so as to ensure that the wave gate is opened only when the target echo arrives and closed when the atmospheric backscattering interference arrives at the angle measurement system. The purpose of removing the backward scattering interference is achieved. The method comprises the steps that in FIG. 4, an echo signal is s (t) (a signal after a wave gate) and a backscattering and target echo is r (t) (a signal before the wave gate) are acquired at an input end of high-speed acquisition; FIG. 4 illustrates the closing of the wave gate upon arrival of the captured backscatter, with no backscatter signal in the signal after the wave gate; the gate opens just before the echo signal is coming, and the signal after the gate is the echo signal.

Claims (1)

1. A method for resisting backscatter using a laser goniometer system, comprising the steps of:
step 1, a laser emits laser pulses with the period of 50ms, and the optical device of the angle measurement system receives backward scattering and target echo signals through atmospheric attenuation and target diffuse reflection;
step 2, the processor of the angle measurement system performs waveform matching on the high-speed collected signals to search for target signals, at the moment, the wave gate is in an open state, the optical signals received by the optical device of the angle measurement system are converted into digital signals by the high-speed collection circuit after photoelectric processing of the detector, and the processor performs waveform matching on the obtained digital signals
a. If the matching is successful, closing the wave gate and simultaneously starting a timer;
a filter is defined by the impulse response h (t) and taken
h(t)=s(-t),-T≤t≤0
For a received signal r (T) to be processed at 0.ltoreq.t.ltoreq.T, the response of the matched filter is:
this gives:
wherein S is a test statistic, that is, the output S of the correlation receiver is the result of sampling the output of the matched filter at the starting point t=0 of the observation area; u is the integral of t, t is the variable, u is the integral;
the actual target echo signal s (t) is a discrete digital sequence s (n) after high-speed acquisition, the received signal r (t) is a sequence r (n), and similarly, the response of the matched filter is as follows:
this gives:
b. if the matching is unsuccessful, continuing to acquire signals to carry out waveform matching;
step 3, after the matching is successful, a timer of the processor counts 49.999ms and then opens a wave gate, the processor processes the signals acquired at high speed to calculate angle information, and at the moment, the backscattering and interference signals are filtered, and only target echo signals are acquired;
step 4, the timer counts up to 50ms Guan Bomen, and the timer restarts counting, and then steps 3 and 4 are repeated continuously.
CN201810779168.5A 2018-07-16 2018-07-16 Laser angle measurement system and anti-backscattering method Active CN109283548B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810779168.5A CN109283548B (en) 2018-07-16 2018-07-16 Laser angle measurement system and anti-backscattering method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810779168.5A CN109283548B (en) 2018-07-16 2018-07-16 Laser angle measurement system and anti-backscattering method

Publications (2)

Publication Number Publication Date
CN109283548A CN109283548A (en) 2019-01-29
CN109283548B true CN109283548B (en) 2024-02-09

Family

ID=65182930

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810779168.5A Active CN109283548B (en) 2018-07-16 2018-07-16 Laser angle measurement system and anti-backscattering method

Country Status (1)

Country Link
CN (1) CN109283548B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110471073B (en) * 2019-09-25 2023-06-16 浙江缔科新技术发展有限公司 Light quantum angle measurement telescope and angle measurement method
CN111273309B (en) * 2020-03-11 2023-04-07 西安应用光学研究所 Method for obtaining target distance

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6138944A (en) * 1999-04-16 2000-10-31 The United States Of America As Represented By The Secretary Of The Army Scatterider guidance system for a flying object based on maintenance of minimum distance between the designating laser beam and the longitudinal axis of the flying object
RU106759U1 (en) * 2011-02-14 2011-07-20 Государственное образовательное учреждение высшего профессионального образования Томский государственный университет (ТГУ) REVERSE SCATTERING SUPPRESSION DEVICE IN THE NEAR ZONE OF POLARIZATION LIDAR
CN103148744A (en) * 2013-01-30 2013-06-12 中国航天空气动力技术研究院 Method for resisting backward dispersion for laser semi-active seeker
CN106688329B (en) * 2009-10-29 2013-07-24 中国航天空气动力技术研究院 Unmanned plane Semi-active LASER target seeker back scattering disturbance restraining method
CN103983145A (en) * 2014-05-21 2014-08-13 中国航天空气动力技术研究院 Method for capturing object by using last pulse policy of laser seeker of unmanned aerial vehicle
CN104330804A (en) * 2014-11-07 2015-02-04 扬州天目光电科技有限公司 Facula tracker and object identification and tracking method using same
CN104820223A (en) * 2015-04-10 2015-08-05 中国科学院上海光学精密机械研究所 Optical field matching filtering range finding device based on M-sequence phase coding

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6138944A (en) * 1999-04-16 2000-10-31 The United States Of America As Represented By The Secretary Of The Army Scatterider guidance system for a flying object based on maintenance of minimum distance between the designating laser beam and the longitudinal axis of the flying object
CN106688329B (en) * 2009-10-29 2013-07-24 中国航天空气动力技术研究院 Unmanned plane Semi-active LASER target seeker back scattering disturbance restraining method
RU106759U1 (en) * 2011-02-14 2011-07-20 Государственное образовательное учреждение высшего профессионального образования Томский государственный университет (ТГУ) REVERSE SCATTERING SUPPRESSION DEVICE IN THE NEAR ZONE OF POLARIZATION LIDAR
CN103148744A (en) * 2013-01-30 2013-06-12 中国航天空气动力技术研究院 Method for resisting backward dispersion for laser semi-active seeker
CN103983145A (en) * 2014-05-21 2014-08-13 中国航天空气动力技术研究院 Method for capturing object by using last pulse policy of laser seeker of unmanned aerial vehicle
CN104330804A (en) * 2014-11-07 2015-02-04 扬州天目光电科技有限公司 Facula tracker and object identification and tracking method using same
CN104820223A (en) * 2015-04-10 2015-08-05 中国科学院上海光学精密机械研究所 Optical field matching filtering range finding device based on M-sequence phase coding

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
一种激光半主动导引头高集成数字处理机的实现;彭晶晶 等;空天防御;第1卷(第3期);20-25 *

Also Published As

Publication number Publication date
CN109283548A (en) 2019-01-29

Similar Documents

Publication Publication Date Title
CN106772404B (en) Laser radar ranging device and method
CN108490410B (en) Two-coordinate radar sea target joint detection and tracking method
US6043867A (en) Tracking system that includes means for early target detection
CN103499819B (en) Measuring device and method for target line-of-sight angel offset and distance
CN109631673B (en) Semi-active laser detection method and system
US6111241A (en) Semi-active laser last pulse logic seeker utilizing a focal plane array
CA2698111C (en) Clutter rejection in active object detection systems
CN103148744B (en) Method for resisting backward dispersion for laser semi-active seeker
CN109283548B (en) Laser angle measurement system and anti-backscattering method
CN103983145B (en) A kind of method utilizing unmanned plane laser seeker most end pulse strategy target acquisition
US20060238411A1 (en) System and method for spatially diverse radar signal processing
JP5551169B2 (en) All-digital line-of-sight (LOS) processor architecture
ES2671613T3 (en) Long range telemetry of small target
US20040051859A1 (en) Programmable pulse capture device with automatic gain control
CN106054205A (en) Laser range finding device and laser range finding method thereof
US20150369918A1 (en) Laser alignment and tracking system
CN207601308U (en) A kind of laser ranging system
EP3571520A1 (en) Method and apparatus for variable time pulse sampling
CN103995259A (en) Radar target adaptive filtering fusion detection method in intensive interference environment
CN105842688A (en) Air target quick capturing method of monopulse radar
CN111257900A (en) Laser radar ranging method and device
CN114047523A (en) Method for detecting and tracking real target by puzzling and disturbing electromagnetic waves based on noise interference
CN109633624A (en) RGPO distinguishing disturbance method based on filtering data processing
CN109696670B (en) Detection and processing device for sniper of robot
CN115480240A (en) Multi-sensor cooperative detection method for small unmanned aerial vehicle

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20240401

Address after: 710000, 7th Floor, Satellite Building, Park, No. 70 Jinye Road, High tech Zone, Xi'an City, Shaanxi Province

Patentee after: Xi'an Raytheon Defense Technology Co.,Ltd.

Country or region after: China

Address before: 710000 two, 1 unit, 1 Jinye Road, 70 High-tech Zone, Xi'an, Shaanxi.

Patentee before: Sun Hongyu

Country or region before: China

TR01 Transfer of patent right